翻訳と辞書 |
Kestrel KL-1 : ウィキペディア英語版 | Kestrel KL-1 __NOTOC__
The Kestrel KL-1 is an American single-engined four-seat utility aircraft designed and built in the 1990s by the Kestrel Aircraft Company of Norman, Oklahoma. ==Design and development== The KL-1 is a composite fuselage cantilever high-wing cabin monoplane designed to meet the requirements of the utility and normal categories of Part 23 of the Federal Aviation Regulations.〔 It had a fixed tricycle landing gear and a conventional four-seat cabin layout.〔 The prototype designated KL-1A and registered ''N960KA'' first flew on 19 November 1995 and was powered by a Lycoming O-320-D2G piston engine driving a two-bladed fixed pitch propeller.〔 A number of improved variants of the KL-1 were planned including an armed observation or forward air control version with underwing weapon pylons.〔 While the prototype was test flying to gain certification the programme was abandoned.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Kestrel KL-1」の詳細全文を読む
スポンサード リンク
翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|